GB1149435A - Method of homing and guiding flying bodies - Google Patents
Method of homing and guiding flying bodiesInfo
- Publication number
- GB1149435A GB1149435A GB32215/67A GB3221567A GB1149435A GB 1149435 A GB1149435 A GB 1149435A GB 32215/67 A GB32215/67 A GB 32215/67A GB 3221567 A GB3221567 A GB 3221567A GB 1149435 A GB1149435 A GB 1149435A
- Authority
- GB
- United Kingdom
- Prior art keywords
- inertial navigation
- flying
- landing
- navigation system
- homing
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired
Links
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
- G01C25/00—Manufacturing, calibrating, cleaning, or repairing instruments or devices referred to in the other groups of this subclass
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41G—WEAPON SIGHTS; AIMING
- F41G7/00—Direction control systems for self-propelled missiles
- F41G7/20—Direction control systems for self-propelled missiles based on continuous observation of target position
- F41G7/30—Command link guidance systems
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41G—WEAPON SIGHTS; AIMING
- F41G7/00—Direction control systems for self-propelled missiles
- F41G7/34—Direction control systems for self-propelled missiles based on predetermined target position data
- F41G7/36—Direction control systems for self-propelled missiles based on predetermined target position data using inertial references
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
- G01C21/00—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00
- G01C21/10—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration
- G01C21/12—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration executed aboard the object being navigated; Dead reckoning
- G01C21/16—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration executed aboard the object being navigated; Dead reckoning by integrating acceleration or speed, i.e. inertial navigation
- G01C21/165—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration executed aboard the object being navigated; Dead reckoning by integrating acceleration or speed, i.e. inertial navigation combined with non-inertial navigation instruments
- G01C21/1652—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration executed aboard the object being navigated; Dead reckoning by integrating acceleration or speed, i.e. inertial navigation combined with non-inertial navigation instruments with ranging devices, e.g. LIDAR or RADAR
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
- G01S1/00—Beacons or beacon systems transmitting signals having a characteristic or characteristics capable of being detected by non-directional receivers and defining directions, positions, or position lines fixed relatively to the beacon transmitters; Receivers co-operating therewith
- G01S1/02—Beacons or beacon systems transmitting signals having a characteristic or characteristics capable of being detected by non-directional receivers and defining directions, positions, or position lines fixed relatively to the beacon transmitters; Receivers co-operating therewith using radio waves
Landscapes
- Engineering & Computer Science (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Chemical & Material Sciences (AREA)
- General Engineering & Computer Science (AREA)
- Combustion & Propulsion (AREA)
- Automation & Control Theory (AREA)
- Computer Networks & Wireless Communication (AREA)
- Manufacturing & Machinery (AREA)
- Radar Systems Or Details Thereof (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Navigation (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Abstract
1,149,435. Inertial navigation. DORNIER SYSTEM G.m.b.H. July 13, 1967 [Nov.26, 1966], No. 32215 /67. Heading G1C. Flying bodies equipped with inertial navigation are guided shortly before landing to the desired landing spot by compensating and correcting the inertial navigation system for drift from a ground station which by taking bearings establishes the actual position of the body and by comparison with the position given by the inertial navigation system calculates a correction value which is used to effect correction of the position of the body. The invention is described as being used with a secondary radar system employing a transponder on the flying body to determine the actual position of the body, this being compared with the position given by the inertial navigation system in a computer. The computer generates a correction signal which is transmitted to the flying body to control a flight programming device thereon. In this way the landing of the flying body can be controlled to facilitate its recovery. A primary radar may be used in place of the secondary radar if desired but the latter is preferred.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DED0051655 | 1966-11-26 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1149435A true GB1149435A (en) | 1969-04-23 |
Family
ID=7053544
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB32215/67A Expired GB1149435A (en) | 1966-11-26 | 1967-07-13 | Method of homing and guiding flying bodies |
Country Status (4)
Country | Link |
---|---|
US (1) | US3456255A (en) |
DE (1) | DE1548415B2 (en) |
FR (1) | FR1555695A (en) |
GB (1) | GB1149435A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20160047629A1 (en) * | 2013-03-20 | 2016-02-18 | Mbda France | Method and device for improving the inertial navigation of a projectile |
Families Citing this family (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2805628A1 (en) * | 1978-02-10 | 1979-08-16 | Teldix Gmbh | METHOD OF DETERMINING THE DRIFT OF A GYRO |
DE3661447D1 (en) * | 1986-03-03 | 1989-01-19 | Litef Gmbh | Navigation method |
US4783744A (en) * | 1986-12-08 | 1988-11-08 | General Dynamics, Pomona Division | Self-adaptive IRU correction loop design interfacing with the target state estimator for multi-mode terminal handoff |
DE4223531C2 (en) * | 1992-07-17 | 1994-10-20 | Bodenseewerk Geraetetech | Device for guiding a powered missile shot from a launcher |
US20090177339A1 (en) * | 2005-03-03 | 2009-07-09 | Chen Robert H | Optimization and Mechanization of Periodic Flight |
Family Cites Families (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3008668A (en) * | 1955-06-06 | 1961-11-14 | Bell Telephone Labor Inc | Guidance control system |
US3028592A (en) * | 1957-06-27 | 1962-04-03 | Gen Precision Inc | Doppler inertial navigation data system |
-
1966
- 1966-11-26 DE DE19661548415 patent/DE1548415B2/en active Pending
-
1967
- 1967-07-13 GB GB32215/67A patent/GB1149435A/en not_active Expired
- 1967-11-10 FR FR1555695D patent/FR1555695A/fr not_active Expired
- 1967-11-21 US US684736A patent/US3456255A/en not_active Expired - Lifetime
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20160047629A1 (en) * | 2013-03-20 | 2016-02-18 | Mbda France | Method and device for improving the inertial navigation of a projectile |
US9534869B2 (en) * | 2013-03-20 | 2017-01-03 | Mbda France | Method and device for improving the inertial navigation of a projectile |
Also Published As
Publication number | Publication date |
---|---|
DE1548415B2 (en) | 1971-12-16 |
DE1548415A1 (en) | 1969-04-17 |
US3456255A (en) | 1969-07-15 |
FR1555695A (en) | 1969-01-31 |
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